Unformatted text preview: V ? Explain your method to determine this from the results of part 1. 3. Approximately how far beyond the wingtip is the upwash in excess of 1% of V ? Explain your method to determine this from the results of part 1. Note: the real 737-800 has a swept and tapered wing which requires more detailed modeling than a single horseshoe vortex. Also, the cruise Mach number of 0.785 is in the compressible subsonic regime which we will address the last week or two of the semester. Nevertheless, I wanted some “real numbers” for you to observe in the results. The results will be approximate and in the right order of magnitude....
View Full Document
- Fall '09
- Aerodynamics, Wingtip vortices, horseshoe vortex, single horseshoe vortex, compressible subsonic regime